View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 34040U 93036JB 22228.49435826 .00000515 00000-0 44974-3 0 9991
2 34040 73.9576 261.9082 0353173 95.9058 268.2420 13.62785696670275
Epoch (UTC): | 16 August 2022 11:51:52 |
Eccentricity: | 0.0353173 |
inclination: | 73.9576° |
perigee height: | 764 km |
apogee height: | 1287 km |
right ascension of ascending node: | 261.9082° |
argument of perigee: | 95.9058° |
revolutions per day: | 13.62785696 |
mean anomaly at epoch: | 268.2420° |
orbit number at epoch: | 67027 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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